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30篇 您的检索式:作者名="TISCHLER M B"
    题名 作者 年代 出处 被引量
1System identification modeling of a small scale unmanned rotorcraft for flight control design 显示文摘Mettler B Tischler M Kanade T 2002Jounal of the American Helicopter Society2002,47,1:1
2System identification of small-size unmanned rotorcraft for control design显示文摘Mettler B Tischler M B Kanada T 2002Journal of the American Helicopter Society2002,47,1:1
3Frequency-response method for rotorcraft system identification: flight applications to BO-105 coupled rotor fuselage dynamics 显示文摘Tischler M B Cauffman M G 1992Journal of the American Helicopter Society1992,37,3:1
4Rapid frequency- domain modeling methods for unmanned aerial vehicle flight control applications 显示文摘Theodore C R Tischler M B Colbourne J D 2004Journal of Aircraft (S0021-8669)2004,41,4:1
5Forward flight trim calculation and frequency response validation of a high-order helicopter simulation model显示文摘Kim F D Celi R Tischler M B 1993Journal of Aircraft1993,30,6:1
6Rapid frequency- domain modeling methods for unmanned aerial vehicle flight control applications 显示文摘Theodore C R Tischler M B Colbourne J D 2004Journal of Aircraft2004,41,4:1
7Rapid frequency - domain modeling methods for unmanned aerial vehicle flight control applications显示文摘C R Theodore M B Tischler J D Colboume 2004Journal of Aircraft2004,41,4:1
8System Identification Modeling of a Small--scale Unmanned Rotorcraft for Flight Control Design显示文摘Mettler B Tischler M Kanade T 2002Journal of the American Helicopter Society2002,47,1:1
9Assessment of Digital Flight Control Technology for Advanced Combat Rotorcraft显示文摘 1989Journal of the American Helicopter Society1989,,:1
10Empirically derived helicopter response model and control system requirements for flight in turbulence显示文摘Lusardi J A Tischler M B Blanken C L 2004Journal of the American Helicopter Society2004,49,3:1
11A multi-disci- plinary flight control development environment and its applica- tion to a helicopter显示文摘Tischler M B Colbourne J D Morel M R 1999Control Systems IEEE1999,19,4:1
12Rapid frequency-domain modeling methods for unmanned aerial vehicle flight control applications显示文摘Theodore C R Tischler M B Colbourne J D 0,,04:1
13Rapid frequency-domain modeling methods for unmanned aerial vehicle flight control applications显示文摘THEODORE C R TISCHLER M B COLBOURNE J D 2004Journal of aircraft2004,41,4:1
14System identification requirements for high- bandwidth rotorcraft flight control system design 显示文摘TISCHLER M B 1990Journal of Guidance Control Dynamics1990,13,5:1
15Identification and verification of frequency- domain models for XV-15 tilt-rotor aircraft dynamics in cruising flight 显示文摘Tischler M B 1986Journal of Guidance Control and Dy- namics1986,9,4:1
16Frequeney-response method for rotorcraft system identification:flight application to BO-105 coupled rotor/fuselage dynamics 显示文摘Tischler M B M G Cauffman 1992Joumal of the American Helicopter Society1992,37,3:1
17Rapid fre- quency-domain modeling methods for unmanned aerial vehicle flight control applications 显示文摘Theodore C R Tischler M B Colbourne J D 2004Journal of Aircraft2004,41,4:1
18Assessment of digital flight-control technology for advanced combat rotorcraft 显示文摘 1989J Am Helicopter Soc1989,34,10:1
19Frequency-response method for rotorcraft system identification:flight application to BO-105 coupled rotor/fuselage dynamics显示文摘Tischler M B Cauffman M G 1992Journal of the American Helicopter Society1992,37,3:1
20System identification model of small scale unmanned rotorcraft for control design 显示文摘Metteler B Tischler M B Kanade T 2002Journal of The American Helicopter Society2002,47,1:1
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